A method for preparing silicon substrate having average crystallite size greater than or equal to 20 μm, including at least the steps of: (i) providing polycrystalline silicon substrate of which average grain size is less than or equal to 10 μm; (ii) subjecting substrate to overall homogeneous plastic deformation, at temperature of at least 1000° C.; (iii) subjecting substrate to localized plastic deformation in plurality of areas of substrate, called external stress areas, spacing between two consecutive areas being at least 20 μm, local deformation of substrate being strictly greater than overall deformation carried out in step (ii); step (iii) being able to be carried out subsequent to or simultaneous to step (ii); and (iv) subjecting substrate obtained in step (iii) to recrystallization heat treatment in solid phase, at temperature strictly greater than temperature used in step (ii), in order to obtain desired substrate.

A method for preparing silicon substrate having average crystallite size greater than or equal to 20 μm, including at least the steps of: (i) providing polycrystalline silicon substrate of which average grain size is less than or equal to 10 μm; (ii) subjecting substrate to overall homogeneous plastic deformation, at temperature of at least 1000° C.; (iii) subjecting substrate to localized plastic deformation in plurality of areas of substrate, called external stress areas, spacing between two consecutive areas being at least 20 μm, local deformation of substrate being strictly greater than overall deformation carried out in step (ii); step (iii) being able to be carried out subsequent to or simultaneous to step (ii); and (iv) subjecting substrate obtained in step (iii) to recrystallization heat treatment in solid phase, at temperature strictly greater than temperature used in step (ii), in order to obtain desired substrate.

A rare earth halide scintillation material the chemical formula of the material being CeBr.sub.3+x, wherein 0.0001x0.1. The rare earth halide scintillation material has excellent scintillation properties including high light output, high energy resolution, and fast decay.

The problem to addressed by the present invention is that of providing a novel technique that can remove a strained layer introduced into a silicon carbide substrate by laser processing. The present silicon carbide substrate manufacturing method involves a processing step for performing laser processing to remove part of a silicon carbide substrate by irradiating the silicon carbide substrate with a laser, and a strained layer removal step for removing a strained layer that was introduced in the silicon carbide substrate by the aforementioned processing step involving heat treatment of the silicon carbide substrate. In this way, the present invention, which is a method of removing a strained layer introduced into a silicon carbide substrate by laser processing, involves a strained layer removal step for heat treating the silicon carbide substrate.

Provided is a method of manufacturing an epitaxial wafer, which includes vapor-phase growing an epitaxial layer on a substrate W placed on a susceptor 3 in a state where an upper surface 4b1 of a lift pin 4 inserted in a through-hole H of the susceptor 3 retracts or projects with respect to an upper opening H1a of the through-hole H. A level difference D from the upper surface 4b1 of the lift pin 4 to the opening H1a of the through-hole H is measured with laser light, and outputs, during epitaxial growth, of heaters 9 located above and beneath the susceptor 3 are adjusted on the basis of the measured level difference D. Thus, a method of manufacturing an epitaxial wafer, which facilitates adjustment of the outputs of the heat sources during epitaxial growth, is provided.

Provided is a method of manufacturing an epitaxial wafer, which includes vapor-phase growing an epitaxial layer on a substrate W placed on a susceptor 3 in a state where an upper surface 4b1 of a lift pin 4 inserted in a through-hole H of the susceptor 3 retracts or projects with respect to an upper opening H1a of the through-hole H. A level difference D from the upper surface 4b1 of the lift pin 4 to the opening H1a of the through-hole H is measured with laser light, and outputs, during epitaxial growth, of heaters 9 located above and beneath the susceptor 3 are adjusted on the basis of the measured level difference D. Thus, a method of manufacturing an epitaxial wafer, which facilitates adjustment of the outputs of the heat sources during epitaxial growth, is provided.

The present invention is a method for manufacturing a substrate for a solar cell composed of a single crystal silicon, including the steps of: producing a silicon single crystal ingot; slicing a silicon substrate from the silicon single crystal ingot; and subjecting the silicon substrate to low temperature thermal treatment at a temperature of 800° C. or more and less than 1200° C., wherein the silicon single crystal ingot or the silicon substrate is subjected to high temperature thermal treatment at a temperature of 1200° C. or more for 30 seconds or more before the low temperature thermal treatment. As a result, it is possible to provide a method for manufacturing a substrate for a solar cell that can prevent decrease in the minority carrier lifetime of the substrate even when the substrate has higher oxygen concentration.

In various embodiments, single-crystal aluminum nitride boules and substrates have low Urbach energies and/or absorption coefficients at deep-ultraviolet wavelengths. The single-crystal aluminum nitride may function as a platform for the fabrication of light-emitting devices such as light-emitting diodes and lasers.

In various embodiments, single-crystal aluminum nitride boules and substrates have low Urbach energies and/or absorption coefficients at deep-ultraviolet wavelengths. The single-crystal aluminum nitride may function as a platform for the fabrication of light-emitting devices such as light-emitting diodes and lasers.

A method for manufacturing a blade, the method includes casting a nickel alloy blade precursor having an airfoil and a root. The airfoil and the root are solution heat treating differently from each other. After the solution heat treating, the root is wrought processed. After the wrought processing, an exterior of the root is machined.